...Naren Shankar R.; Ganesan V.G. Purpose The purpose of this study is to analyse numerically and experimentally the effects of lip thickness (LT) and bypass ratio on co-flowing nozzle under subsonic and correctly expanded sonic jet decay at different Mach numbers. Design/methodology/approach Co...

...Sathish Kumar K; Naren Shankar R; Anusindhiya K; Senthil Kumar B.R. Purpose This study aims to present the numerical study on supersonic jet mixing characteristics of the co-flow jet by varying lip thickness (LT). The LT chosen for the study is 2 mm, 7.75 mm and 15 mm. Design/methodology...

...Naren Shankar R.; Ganesan V.G.; Dilip Raja N.; Sathish Kumar K.; Vijayaraja K. Purpose The effect of increasing lip thickness (LT) and Mach number on subsonic co-flowing Jet (CFJ) decay at subsonic and correctly expanded sonic Mach numbers has been analysed experimentally and numerically...

...Naren Shankar R.; Kevin Bennett S.; Dilip Raja N.; Sathish Kumar K. Purpose This study aims to analyze co-flowing jets (CFJs) with constant velocity ratio (VR) and varying primary nozzle lip thickness (LT) to find a critical LT in CFJs below which mixing enhances and beyond which mixing inhibits...

...Naren Shankar R.; Kevin Bennett S. Purpose Subsonic commercial aircraft operate with turbo-fan engines that operate with moderate bypass ratio (BR) co-flowing jets (CFJ). This study aims to analyse CFJ with constant BR 6.3 and varying primary nozzle lip thickness (LT) to find a critical LT in CFJ...